AS 311 Engine Presentation PW-120_121 (1)

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Embry-Riddle Aeronautical University *

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311

Subject

Mechanical Engineering

Date

Apr 3, 2024

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docx

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1

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1. Give two examples of aircraft in which this engine is used. ATR 42-400, De Havilland Aircraft Dash 8-100 2. What is the general type of engine? (Turboprop, turboshaft, turbojet, turbofan) Turboprop 3. Describe the inlet using any of the following features that are present: 1. divergent 2. fixed geometry 3. Variable inlet guide vanes (VIGV) 4. Inertial (particle) separator 5. 4.5 :1 6. Mixed bypass/exhaust flow 4. Describe the compressor using any of the following features that are present: 1. Centrifugal blisk 1. 2 stages, 1 on each shaft 2. 3 shafts (N1, N2, Free power) 3. Counter rotating, as far as I can tell 5. Describe the combustor using any of the following features that are present: 1. Reverse flow 2. Single-annular, dual-annular, or twin-annular-premixing-swirler injectors 6. Describe the turbine using any of the following features that are present: 1. 2 turbine power stages, free turbine, shrouded blades 2. Turbine exit guide vanes 3. Turbine blade cooling methods 7. Describe the exhaust section and thrust reversers using any of the following features that are present: 1. Exhaust duct shape divergent Fixed 2. Mixed exhaust and bypass airflow 3. clamshell-type /located on the rear of the engine nacelle 4. Reverse flow combustor
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